IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 IRIDIUM 106
1 41917U 17003A 25314.85956223 .00000063 00000-0 15590-4 0 9991
2 41917 86.4013 179.7619 0001602 88.7720 271.3659 14.34216875461912Epoch: 2025-11-10T20:37Z
TLE epoch observation values (Epoch: 2025-11-10T20:37:46.176Z)
Latitude
-0.00007°
Longitude
-179.93492°
Altitude
780.694 km
Speed
7.464 km/s
True Right ascension
11h 59m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:33:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.78 km
Perigee altitude
773.489 km
Semi-major axis
7,152.771 km
Eccentricity
0.00016
Inclination
86.4013°
RAAN
179.7619°
Arg. of periapsis
88.772°
True anomaly
271.34755°
Mean anomaly
271.3659°
Eccentric anomaly
271.35672°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00001559
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-11 15:09:22.067Z | 156.282° SSE | 2025-11-11 15:14:22.067Z | 76.445° E | 34.445° | 2025-11-11 15:18:22.067Z | 18.44° NNE |
| 6 mins | 2025-11-11 16:52:22.067Z | 246.852° WSW | 2025-11-11 16:55:22.067Z | 289.183° WNW | 18.879° | 2025-11-11 16:58:22.067Z | 326.862° NNW |
| 8 mins | 2025-11-12 03:21:22.067Z | 354.015° N | 2025-11-12 03:25:22.067Z | 241.701° WSW | 44.402° | 2025-11-12 03:29:22.067Z | 184.2° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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